A technique for detecting defects in aircraft wiring, such as for detecting partial discharges or arcing in wiring or cables is disclosed. A high frequency current transformer (HFCT) is fixingly positioned in contact with a wire so that the wire is encircled by the HFCT. partial discharges from a damaged wire so encircled will induce a current in the HFCT proportional to the current of the discharge. The HFCT includes a conductive coil-like pattern formed onto a flexible insulating material. The insulating material has slits between each coil-turn. The HFCT also includes a core of flexible material fitted between the coil-turns through the slits.
|
1. A high frequency current transformer (HFCT) for detecting partial discharges produced by faulty or damaged cables and wires, said HFCT comprising:
at least one conductive coil-like pattern formed onto a flexible insulating material, said insulating material having slits between each coil-turn of the coil-like pattern; and
a core of flexible material fitted between the coil-turns through said slits while permitting said flexible insulating material to remain substantially flat to form a flat flexible current transformer, said core enhancing and directing flux induced in the coil-like pattern.
14. A method for fabricating a high frequency current transformer (HFCT) for detecting partial discharges produced by faulty or damaged cables and wires, said method comprising the steps of:
producing one or more highly conductive coil-like patterns, each pattern having a plurality of coil turns, on a flexible insulating material;
incising said flexible insulating material between each of the plurality of coil-turns of the coil-like patterns; and
interlacing a flexible core material through said incisions while permitting said flexible insulating material to remain substantially flat to form a flat flexible current transformer, said flexible core material enhancing and directing flux induced in the coil-like patterns.
8. A system for detecting partial discharges produced by faulty or damaged cables and wires, the system comprising:
at least one high frequency current transformer (HFCT) comprising at least one conductive coil-like pattern formed onto a flexible insulating material, said insulating material having slits between each coil-turn of the coil-like pattern; and a core of flexible material fitted between the coil-turns through said slits, said core enhancing and directing flux induced in the coil-like pattern;
a housing dimensioned for mounting said at least one HFCT around a wire or wire-bundle and for supporting said at least one HFCT in close proximity to said wire or wire bundle; and
a processor in electrical communication with said at least one HFCT, said processor configured for analyzing electrical signals produced by, and received from said at least one HFCT.
2. The HFCT of
3. The HFCT of
4. The HFCT of
5. The HFCT of
6. The HFCT of
9. The system of
10. The system of
11. The system of
12. The system of
13. The system of
15. The method of
16. The method of
17. The method of
|
This invention was made with Government support under Contract No. N00014-02-C-0402 awarded by the Office of Naval Research. The Government has certain rights in this invention.
This disclosure relates generally to systems and methods for detecting defects in aircraft wiring, and more particularly, to systems and methods for detecting partial discharges or arcing in wiring or cables.
Wiring is a critical system in aircraft, shipboard, industry and home applications. Aircraft wiring integrity and safety related issues are known to be serious and have received a great deal of interest after the Swissair 111 and TWA 800 accidents. Also, electrical fires in industry account for a large portion of property loss, and electrical fires in the home is a significant portion of the fires occurring in the home that threaten life and damage property.
Aircraft wiring insulation is much thinner than that found in building wiring in order to reduce weight. This thin insulation deteriorates with age due to changes in chemical composition, vibration during flights, large temperature changes, and exposure to agents such as dust, salt, moisture and cleaning chemicals. This wiring is also exposed to other mechanical stresses during maintenance. The aforementioned effects will degrade the insulation, causing cracks and chafing. These insulation defects can cause arcing between wires or surrounding metals. Humidity together with salt and dust depositions can make the arc creation more probable.
The detection of aircraft wiring defects is primarily performed by visual inspection by maintenance personnel. This manual inspection is a slow process and its reliability is not satisfactory. Furthermore, as it requires twisting the wiring in order to check chafing, this visual inspection often causes more problems than it can identify. Therefore, a need exists for techniques, to detect defects in wiring or cables, that can be perform by other than visual inspection and will not cause further degradation to the wire or cable under test.
Partial discharge signal detection can be used to characterize the condition of wiring. If a partial discharge occurs, the discharge will generate high frequency electrical signals traveling along the cable. This high frequency electrical signal can be detected with high frequency current transformers (HFCTs). The commercially available current transformers are typically large and heavy and can not be used for aircraft wiring monitoring as a permanently installed sensor.
Partial discharge (PD) testing is a sensitive, widely used method to characterize the condition of insulation materials. The high frequency electrical signal generated by the PD activity can be detected with broadband, high frequency current transformers (HFCT). In the various embodiments of the present disclosure, current transformer designs are described suitable for retrofitting onto wires and cable bundles. Integration of several miniature current transformers into a connector, or for retrofit applications into a connector-middle piece is also described. Further embodiments may also contain preamplifiers and PD signal processing electronics.
According to an aspect of the present disclosure, a high frequency current transformer (HFCT) for detecting partial discharges produced by faulty or damaged cables and wires and a method of fabrication thereof are provided. The HFCT includes at least one conductive coil-like pattern formed onto a flexible insulating material, wherein the insulating material has slits incised between each coil-turn of the coil-like pattern. A core of a flexible material is fitted between the coil turns through said slits.
According to an additional aspect of the present disclosure, a system for detecting partial discharges produced by faulty or damaged cables and wires is provided. The system includes at least one high frequency current transformer (HFCT) configured to detect charge transfers in the range of 10 to 900 pico-Coulombs. The HFCT has a core surrounded by a coil of conducting material. Additionally, a housing dimensioned for mounting the HFCT around a wire, cable or wire-bundle and for supporting said at least one HFCT in close proximity to said wire or wire bundle and a processor in electrical communication with the HFCT, for analyzing electrical signals produced by and received from the HFCT, are provided.
According to another aspect of the present disclosure, a method for fabricating a high frequency current transformer (HFCT) for detecting partial discharges produced by faulty or damaged cables and wires. The method includes the steps of producing one or more highly conductive coil-like patterns, each pattern having a plurality of coil turns, on a flexible insulating material. The flexible insulating material is then incised between each of the plurality of coil-turns of the coil-like patterns. A flexible core material is interlaced through the incisions.
The above and other aspects, features, and advantages of the present invention will become more apparent in light of the following detailed description when taken in conjunction with the accompanying drawings in which:
Preferred embodiments of the present invention will be described hereinbelow with reference to the accompanying drawings. In the following description, well-known functions or constructions are not described in detail to avoid obscuring the invention in unnecessary detail.
The insulation condition of a wire, cable or cable bundle can be tested by partial discharge diagnostics or arcing. Electric discharges that do not completely bridge adjacent electrodes are called partial discharges (PD). The magnitude of such discharges are usually small, the amount of charge transferred is in the range of ten to a few hundred pico-Coulombs, e.g., 10–900 pC. For a partial discharge test, a suitably high AC or DC voltage is applied to conductors surrounding the insulation material under test. Alternatively, the discharge can be detected under normal current/voltage operating conditions depending on the defect and energized system characteristics. If partial discharge occurs, the discharge will generate high frequency electrical signals traveling along the cable. This high frequency electrical signal can be detected with high frequency current transformers (HFCTs).
The basic principle for current transformer based AC current measurement is illustrated in
The alternating current (I) in the wire 102 will induce an alternating magnetic field in the magnetic core 101. This magnetic field in the core 101 will induce voltage in the coil 103, which is proportional to the current (I) in the wire 102.
A current signal generated by a partial discharge can be detected with a single HFCT around the cable bundle, or similarly, a smaller size HFCT can be used around a single wire. The current sensor of the present disclosure, preferably, has a flat design, so as not to significantly increase the diameter of the wire. Additionally, the HFCT is constructed in a manner suitable for installation and/or clamping onto a wire, cable or wire bundle to allow installation onto assembled cable harnesses, or alternatively, can be installed and fixed onto wires, wherein both wire ends have already been connected.
Referring to
For proper functioning of the HFCT 300, the magnetic core 301 is configured to form a closed cylinder. The wire coil 201, however, is not required to form a completely closed cylinder, though the optimal form is a closed cylinder.
Preferably, the core material 301 is a flexible, thin, high permeability material, useable for frequencies up to 500 MHz or even higher. Materials such as Cobalt-based amorphous metal and Ferrite Polymer Composite (FPC) Films may be used, as well as, cores with unity permeability, such as plastic. Several layers can be stacked to achieve the desired core size but still retain the flexibility. Overlapping the ends of the core layer during installation will close the magnetic path. Additionally, the core may be an air core, e.g., a Rogowsky coil.
The HFCT 300 may be embedded into a plastic structure. This plastic structure can serve as a mechanical protection and may have a self-locking whole-pin arrangement at the sides for fixing the structure onto the wire. The HFCT 300 can also be pre-formed and tightened onto a wire with a shrink-tube outer cover or other technique.
Additionally, a preamplifier or other signal processing chips/circuitry can be directly mounted onto the HFCT 300 itself. The additional circuitry can provide some or all of the functionality of the remote signal processing system 404, thus, providing a signal amplification and/or analysis in a self-contained and compact device. Further, circuitry for wireless communications, utilizing standard protocols such as bluetooth or 802.11a/b/g, can be included, eliminating the need for providing leads 403 to transmit the signals to a central processor or display.
The HFCT can be shielded by applying a conductive shield around the HFCT to reduce noise generated from surrounding electrical components. Additionally, capacitive voltage sensors can be used as a secondary method of partial discharge detection which, when used in conjunction with the current transformer, can provide a means of further reducing signal noise by comparing results from both sensors.
In an alternate embodiment, the conductive coil 201 can be directly deposited to the core material 301. If the core 301 is conductive, a suitable insulation layer will be provided to be used under the coil material 301.
Additionally, a HFCT may be integrated to a connector 500 (see
While the disclosure has been illustrated and described in typical embodiments, it is not intended to be limited to the details shown, since various modifications and substitutions can be made without departing in any way from the spirit of the present disclosure. As such, further modifications and equivalents of the disclosure herein disclosed may occur to persons skilled in the art using no more than routine experimentation, and all such modifications and equivalents are believed to be within the spirit and scope of the disclosure as defined by the following claims.
Evers, Nicole Andrea, Sarkozi, Janos Gyorgy
Patent | Priority | Assignee | Title |
10777349, | Oct 23 2017 | Schweitzer Engineering Laboratories, Inc.; Schweitzer Engineering Laboratories, Inc | Current transformer with flexible secondary winding |
10948843, | Jun 12 2017 | Vibrosystm Inc. | Method of monitoring partial discharges in a high voltage electric machine, and connection cable therefore |
10984940, | Dec 10 2018 | Schweitzer Engineering Laboratories, Inc. | Compression housing for a laminate core of an inductive current transformer |
7952360, | Mar 14 2007 | General Electric Company | Method and system for passively detecting and locating wire harness defects |
8466697, | Apr 28 2009 | Lam Research Corporation | Arrangements for detecting discontinuity of flexible connections for current flow and methods thereof |
8502554, | Sep 23 2011 | BAKER HUGHES, A GE COMPANY, LLC | Current transformer assembly for use with electrical monitoring systems and methods of assembling same |
8674682, | Sep 30 2009 | General Electric Company | Monitoring system and current transformers for partial discharge detection |
8816698, | Mar 19 2007 | General Electric Company | System for detecting faults in electrical wiring, and manufacturing method thereof |
Patent | Priority | Assignee | Title |
4621231, | Jun 19 1984 | ABB POWER T&D COMPANY, INC , A DE CORP | Toroidal sensor coil and method |
5386193, | Feb 15 1991 | FUJI ELECTRIC CO , LTD | Partial discharge detecting device for resin-molded transformer |
6067474, | Aug 01 1997 | Advanced Bionics AG | Implantable device with improved battery recharging and powering configuration |
6313640, | Feb 03 1998 | ABB Inc | System and method for diagnosing and measuring partial discharge |
20020130668, | |||
20030151412, | |||
JP57120314, | |||
JP60015905, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Dec 18 2003 | SARKOZI, JANOS GYORGY | General Electric Company | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 014849 | /0641 | |
Dec 19 2003 | EVERS, NICOLE ANDREA | General Electric Company | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 014849 | /0641 | |
Dec 23 2003 | General Electric Company | (assignment on the face of the patent) | / | |||
Jun 11 2004 | General Electric Corporation | NAVY, SECRETARY OF THE, UNITED STATES OF AMERICA | CONFIRMATORY LICENSE SEE DOCUMENT FOR DETAILS | 015952 | /0434 |
Date | Maintenance Fee Events |
Dec 20 2005 | ASPN: Payor Number Assigned. |
Jun 07 2010 | M1551: Payment of Maintenance Fee, 4th Year, Large Entity. |
Jul 18 2014 | REM: Maintenance Fee Reminder Mailed. |
Dec 05 2014 | EXP: Patent Expired for Failure to Pay Maintenance Fees. |
Date | Maintenance Schedule |
Dec 05 2009 | 4 years fee payment window open |
Jun 05 2010 | 6 months grace period start (w surcharge) |
Dec 05 2010 | patent expiry (for year 4) |
Dec 05 2012 | 2 years to revive unintentionally abandoned end. (for year 4) |
Dec 05 2013 | 8 years fee payment window open |
Jun 05 2014 | 6 months grace period start (w surcharge) |
Dec 05 2014 | patent expiry (for year 8) |
Dec 05 2016 | 2 years to revive unintentionally abandoned end. (for year 8) |
Dec 05 2017 | 12 years fee payment window open |
Jun 05 2018 | 6 months grace period start (w surcharge) |
Dec 05 2018 | patent expiry (for year 12) |
Dec 05 2020 | 2 years to revive unintentionally abandoned end. (for year 12) |